Liquid Propulsion Systems: From Payload and Orbit to Design of Rocket Engine Components
During this 1-day seminar, attendees will be introduced to best practices, challenges, considerations, and requirements involved in liquid propulsion system development, illustrated through various case studies diving into component level development highlighting the turbopump and rocket nozzle as examples.
Seminar Outline:
• Requirements for development of liquid propulsion system
• Development of preliminary concept of launcher for specific payload and orbit
• Selection of configuration and design of turbopump
• Detailed design of turbine and pump components
• Secondary flow systems and force analysis
• Rotor dynamics and bearing analysis
• Nozzle sizing and cooling
Who Should Attend:
We are encouraging engineers, designers, project managers, and other technical professionals working in start-ups, government agencies, commercial space companies, and educational intuitions to join us to network and learn more about liquid propulsion systems, from payload and orbit to design of rocket engine components.
* Please note: lunch and morning/afternoon refreshments are included in this event.
Liquid Propulsion Systems: From Payload and Orbit to Design of Rocket Engine Components